N361NC

Part: SKIN — CRACKED (BS 420) · airframe 76,717 hrs · 53,370 cycles

SUBSURFACE CRACK AT BS420+3 AT STR26L. REPAIRED FUSELAGE CRACK IAW 53-00-01 REPAIR 31 FIG. 201

Part: SKIN — CRACKED (BS 400) · airframe 76,717 hrs · 53,370 cycles

SUBSURFACE CRACK AT BS400, EXISTING REPAIR ABOVE STR19R. REMOVED EXISTING REPAIR & REPLACED WITH NEW REPAIR DOUBLER IAW SRM 53-00-01 FIG. 201.

Part: SKIN — CRACKED (BS 500) · airframe 76,717 hrs · 53,370 cycles

SUBSURFACE CRACK AT BS 500+3-BS500+8.5 BELOW STR17R. REPAIRED FUSELAGE CRACK IAW SRM 53-00-01 REPAIR 31 FIG. 201.

Part: FRAME — CRACKED · airframe 75,902 hrs · 51,637 cycles

2 CRACKS FOUND ON BS 727 CORD AT S18A [LEFT HAND]. REPLACED LT CHORD AT STA 727 FROM STR 18A – L TO STR 27L WITH NEW PART (P/N 65C38494-1) IAW SB 737-53A1166 REV 2 AND DWG 65C37277 REV -.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

CRACKED ANGLE ON FLOORBEAM WEB IN E&E BAY AT BS328 LBL 30. FABRICATED MADE REPAIR PART ON FLOORBEAM WEB IN E&E BAY AT STA 328 LBL 30 IAW DRAWING NR 65-45812 REV CR AND SRM 51-30-01 REV 116. INSTALLED ANGLE IAW SRM 51-40-02 REV 116.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,902 hrs · 51,637 cycles

CORRODED INTERCOSTAL AT STA 328 - 344 LBL 10. INSTALLED NEW INTERCOSTAL PART 65-45834-259 AT STA 328 - 344 LBL 10 IAW DRAWING 65-45834 REV B AND SRM 51-40-02 REV 116.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

CRACK ON FRAME 727E BETWEEN S-8L AND S-9L INBOARD FASTENER HOLE. CRACKED FRAME STA 727E BETWEEN STR 8 AND STR 9 LT REPAIRED IAW SB737-53-1216-FIG 8 REV 1.

Part: TIE CLIP — DAMAGED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

DAMAGED STRINGER TIE, AFT LOWER CARGO PIT BILGE AT BS727A S26L. DAMAGED STRINGER TIE, AFT LOWER CARGO PIT BILGE AT STA 727A STR 26L REPLACED WITH MADE REPAIR PART IAW REV 116 SRM 51-30-01 FIG 7, INSTALLED WITH FASTENERS IAW REV 116 SRM 51-40-02 PAR 4 AND 7.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,902 hrs · 51,637 cycles

CORROSION FOUND IN SEAT TRACK AT RBL 62 VARIOUS LOCATIONS BETWEEN STA 500B - 787. CORRODED SEAT TRACK REPLACED WITH MADE REPAIR PART IDENTIFIED IAW CARGO CONVERSION/ IPC REV E SECTION 53-30-52 DETAIL I. FASTENER HOLES DRILLED AND FASTENERS INSTALLED IAW SRM REV 116 SECTION 51- 40-02.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

CRACKED STRINGER CLIP BS277 S22R ACCESSIBLE FROM E&E BAY. INSTALLED STRINGER CLIP PART 69-37411-5 AT STA 277 STR 22R IAW ARM 51-40-02 REV 116 AND DRAWING 65-45805 REV J.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,902 hrs · 51,637 cycles

CORROSION ON UPPER AND LOWER SURFACE OF SHEAR TIE ANGLE ON BS787 S27R. CORRODED SHEAR TIE ANGLE ON STA 787 STR 27R REPLACED WITH MADE REPAIR PART MAT IDENTIFIED IAW SRM REV 116 SECTION 53-60-07 FIG MADE REPAIR PART FABRICATED IAW SAME SRM SECTION 51-30-01 FIG 7 AND INSTALLED WITH RIVETS IAW SECTION 51-40-02.

Part: SKIN — GOUGED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

FOUND DAMAGE GOUGE TO INNER SKIN MACHINED DOUBLER BETWEEN BS380 - 400 AND S21L & 20L. REPAIRED SKIN BETWEEN STA 380-400 STR 21L AND 20L. IAW REPAIR INSTRUCTION DOC CS-23260-009 DATE 11 APR 2018 WHIT NO DEVIATIONS.

Part: SPAR — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 75,902 hrs · 51,637 cycles

CORROSION FOUND ON VERTICAL STABILIZER REAR SPAR RAIL LEFT HAND SIDE OF VERTICAL STABILIZER APPROXIMATELY AT BS1016 AND RS141.52. REPAIRED V-STAB SPAR RAIL, LT SIDE OF V-STAB APPROXIMATELY AT B STATION 1016 AND RUDDER STATION 141.52. IAW SR NUMBER 3-4159366135 REV 21-MAY-2C13. NO DEVIATIONS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

CRACK ON FRAME 480 BETWEEN S-8R AND S-9R INBOARD FASTENER HOLE. CRACKED FRAME STA 480 BETWEEN STR 8R AND 9R REPAIRED IAW SB737-53-1216 REV 1 FIGURE 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

CRACK IN FUS SKIN AT STA 386 STR 26L. CRACK IN FUSE SKIN AT STA 386 STRINGER 26L, REMOVED AND REPAIRED IAW SERVICE REQUEST SR 4-4012174797. RE INSTALLED AND INSPECTED SERVICEABLE.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

CRACKED INTERCOSTAL AT STA 312 BL0. CRACKED INTERCOSTAL AT STA 312 BL0 REPAIRED IAW SRM REV 116 SECTION 53-10-51 REPAIR 10.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

CRACK ON LEFT HAND CORD ON BULKHEAD 178. REPAIRED LT CHORD ON BULKHEAD 178 IAW SB 737-53A1173-AMOC- 01 REV DATED FEB 21 2012.

Part: WEB — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

CRACKS FOUND ON WEB AT BL0 FS 708. CRACKED WEB AT BL0 FSTA 708 REPAIRED IAW REPAIR INSTRUCTION DOC NR C-23260-012 DATED 10 MAY 2018.

Part: WEB — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

MULTIPLE CRACKS ON WEB UNDER SEAT TRACK BS708 LBL 24.82. REPAIRED WEB UNDER SEAT TRACK STA 708 LBL 24.82 IAW REPAIR DOC CS-23260-008 REV A/24 JUNE 2018.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

CRACK FOUND ON THE RT INBOARD CHORD BS 616, BOTTOM FASTENER. CRACKED IB RT CHORD AT BSTA 616 REPAIRED IAW SB 737-53A1254 REV 3 AND REPAIR INSTRUCTION DOC NR CS-26230- 015 DATED 10 JUNE 2013.

Part: WEB — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

CRACKED WEB ON FLOOR STRUCTURE IN AFT CABIN RIGHT HAND SIDE BETWEEN BS1016 AND BS1006 AT RBL 40. FABRICATED MADE REPAIR PART IAW SRM 53-60-51 FIG 1 REV 116 AND SRM 51-30-01 REV 116. INSTALLED WEB IN FLOOR STRUCTURE IN AFT CABIN RT WIDE BETWEEN STA 1016 AND 1006 RBL 40 IAW SRM 51-40-02 REV 116 AND DRAWING NO 65-43812 REV H.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,902 hrs · 51,637 cycles

CORROSION ON BROWN LINE BS791 RBL 45. INSTALLED NEW SEAT TRACK AT STA 791 RBL 45. IAW SRM 51-10-02 PARA 8 PAGE 8 REV 116.

Part: TIE CLIP — MISSING (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

MISSING STRINGER TIE ON BS787 S26R AFT CARGO PIT. AT MISSING STRINGER TIE LOCATION 787 STR 26R NEW FABRICATED PART INSTALLED IAW SRM 51-30-01 FIG 7 AND SRM 51-40-02 PAR 4.7 REV 116.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

GOUGE/TOOLING DAMAGE ON S23R AND STIE AT BS887. INSTALLED NEW STR IN AFT PIT AT STA 847 - 910, STR 23R IAW SRM CH 53-00-03 REV 116 AND IAW B737-300 SRM CH 51-40-02 REV 116.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

CRACK ON FUS SKIN AT BS500B TO 500C BETWEEN 23L & 24L REPAIRED CRACK ON FUSELAGE SKIN AT STA 500B TO 500C BETWEEN STRINGER 23L AND 24L IAW SB 737-53-1168 REV 4 AND SRM REV 116 CHAPTER 53-00-01 REPAIR 31 FIG 201 DETAIL VII.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,902 hrs · 51,637 cycles

CORROSION FOUND ON THE AFT END OF THE FLOOR BEAM AT RBL 24.84 727B WL 208.1. CORROSION ON AFT END OF SEAT TRACK AT RBL 24.84 727B WL 208.1 BLENDED. IAW SRM 51-10-2-14 REV 116. FOUND TO BE BEYOND SRM LIMITS. SEAT TRACK REMOVED AND REPLACED WITH MADE REPAIR PART. MATERIAL IDENTIFIED IAW SRM 53-60-52. SEAT TRACKS INSTALLED WITH FASTENERS IAW SRM 51- 40-2.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

CRACKED ANGLE ON FLOORBEAM WEB IN E&E BAY ST BS344 LBL 12 ON AFT SIDE OF WEB. FABRICATED MADE REPAIR PART FOR CRACKED ANGLE ON FLOORBEAM WEB IAW DRAWING NR 65-45815 REV DK AND SRM 51-30-01 REV 116.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,902 hrs · 51,637 cycles

CORROSION ON FLOORBEAM IN AFT CABIN BS986.5 BETWEEN RBL 0 AND RBL 24.75. REMOVED CORROSION ON FLOORBEAM IN AFT CABIN AT STA 986.5, BETWEEN RBL 0 AND RBL 24.75 IAW SRM REV 51-10-02. FLOOR STRUCTURE IDENTIFIED IAW SRM REV 116 53-60-51. REMOVED 0.027" MATERIAL FROM ORIGINAL 0.125" MATERIAL THICKNESS. MAX ALLOWABLE REMOVAL 15%(0.019"). REMAINING MATERIAL THICKNESS BEYOND ALLOWABLE LIMITS IAW SRM REV 116 53-60-51 (LOWEST READING 0.098"). REPAIRED FLOORBEAM IAW CUSTOMER SERVICE REPAIR CS-23260-016 REV A / 29 JUNE 2018.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

CRACKED STRINGER SPLICE AT BS908, S4R AT RIVET AFT OF STRINGER CLIP. CRACKED STRINGER SPLICE AT STA 908, STR 4R AND STRINGER CLIP REPLACED WITH OEM PARTS. ITEMS IDENTIFIED IAW SB737-53A1322 REV 00 (ORIGINAL) AND INSTALLED IAW SRM REV 116 SECTION 51-40-01

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

R1 UPPER FORWARD CORNER HAS A SUSPECT CRACK AT THE NR 3 HOLE. NDT CONFIRMED MULTIPLE HOLES CRACKED IN SKIN AND BEARSTRAP OF R1 DOOR UPPER FWD CORNER. REPAIRED IAW SR 3-4173028774 AND REPAIR SKETCH KFC-HLH-18-0002-22C.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

CORROSION ON STRINGER 23R BS360 ACCESSIBLE FROM E&E BAY. STRINGER 23R STA 360 ACCESSIBLE FROM E&E BAY AND STRINGER SPLICE 65-9664-12 REPLACED WITH NEW PARTS IAW SRM REV 116 53-00-03 REPAIR 1 AND INSTALLED IAW SRM REV 116 51-40-02.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

LEFT HAND SHEAR WEB HAS A CRACK RUNNING THROUGH THE AFT WEB INB TWO HOLES AT BS 727 STR 18A LEFT HAND. INSTALLED NEW LT SHEAR WEB AT STA 705-727 ST STR 18A. IAW SB 737-53A1166 REV 2, DWG 65C37277 REV -.

Part: WEB — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

MULTIPLE CRACKS FOUND ON WEB UNDER SEAT TRACK AT BS708 RBL 24.82. MULTIPLE CRACKS ON WEB UNDER SEAT TRACK AT STA 708 RBL 24.82 REPAIRED IAW SB 737-57A1296 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

CRACK ON FRAME 787 BETWEEN S-8L AND S-9L INBOARD FASTENER HOLE. CRACKED FRAME AT STA 787 BETWEEN STR 8L AND 9L REPAIRED IAW SB 53-1216 REV 1 FIG 8.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,902 hrs · 51,637 cycles

CORROSION FOUND ON FLOOR SUPPORT UNDER MAIN CABIN AT BS355 RBL 24 (BOTH SIDE OF SUPPORT). ACCESS FROM E&E BAY. REPLACED FLOOR SUPPORT UNDER MAIN CABIN AT STA 355 RBL 24 IAW SRM CHAPTER 51-10-02 PARAGRAPH 8 PAGE 8 REV 116.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

GOUGE ON FLOORBEAM WEB IN E&E BAY AT BS312 LBL 8. REPAIRED FLOORBEAM WEB AT STA 312 LBL 8 IAW DWG 23260.1-053-014-001 REV NC.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,902 hrs · 51,637 cycles

BULGING SKIN FOUND 13" AFT OF STA 727 AT STR 27L. REPLACED 3 KEEL SECTIONS, 2 LT AND 1 RT IAW SRM 53-60-12 REPAIR 3 REV 116, SRM 51-40-02 REV 116.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

CRACKED INTERCOSTAL & ATTACH BRACKET BETWEEN STA 907-927, RBL 53 AT STR 17R. INSTALLED INTERCOSTAL AND BRACKET, FABRICATED REPAIR PART BETWEEN STA 907-927 RBL 53 AT STR 17R IAW SRM 51-30-01 AND 51-40-01 REV 116.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,902 hrs · 51,637 cycles

CORROSION ON SEAT TRACK IN AFT CABIN AT BS1006, RBL 24.75. CORROSION ASSESSED ON SEAT TRACK IN AFT CABIN AT STA 1006 RBL 24.75 FOUND BEYOND LIMITS AS PER SRM, CH 53-00-02 REV 116. SEAT TRACK REPLACED IAW SRM CH 51-10-02 REV 116. HOLES DRILLED IAW SRM CH 51-10-02 REV 116. HOLES COUNTERSUNK IAW SRM CH 51-40-08 REV 116.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,902 hrs · 51,637 cycles

SLIGHT SURFACE CORROSION ON FLOORBEAM BS 328 RBL 12. REPLACED CORRODED FLOORBEAM CAP BS328RBL-RBL 50 IAW SRM 53-10-51 REV 116 FIG 201.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,902 hrs · 51,637 cycles

AFT CARGO COMPARTMENT DOOR UPPER SILL BEAM AND ATTACH ANGLE CORRODED BETWEEN BS807 - BS827. UPPER SILL BEAM WEB CORRODED BEYOND LIMITS PER SRM CH 53-60-15 REV 116. MATERIAL IDENTIFIED PER SRM CH 53-60-15 REV 116. MADE REPAIR PARTS IAW SRM CH 51-30-01 REV 116. FASTENERS IDENTIFIED PER DRAWING 65-47956 REV G. NEW REPAIRED PARTS INSTALLED IAW SRM CH 51- 40-02 REV 116.

Part: ATTACH FITTING — MISSING (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

KEEL BEAM ATTACH CLIP MISSING AT BS787 AFT CARGO PIT. KEEL BEAM ATTACH CLIP AT STA 787 AFT CARGO PIT L/H INSTALLED. MADE REPAIR USED MAT IDENTIFIED IAW SRM REV 116 SECTION 53-00-07. PART FABRICATED IAW SECTION 51-30-01 AND INSTALLED IAW SECTION 533-00-07 FIG 202.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

CRACK FOUND ON THE LT INBOARD CHORD BS 616, BOTTOM FASTENER. REPAIRED LT I/B CHORD BS 616 IAW SB 737- 53A1254 FIG 19 REVISION 3 DTD 13 NOV 2017 WITH NO DEVIATIONS.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

CRACKED STRINGER TIE AT BS927 S24R AFT CARGO PIT. CRACKED STRINGER TIE AT STA 927 STR 24R AFT CARGO PIT REPLACED WITH MADE REPAIR PART IAW REV 116 SRM 51- 30-01 FIG 7, INSTALLED WITH FASTENERS IAW REV 116 SRM 51-40-02 PAR 4 AND 7.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

SUSPECT CRACK ON INBOARD NESTED ANGLE CENTER HOLE AT BS663 UNDER FLOOR. SUSPECTED CRACK ON I/B NESTED ANGLE CENTER HOLE AT STA 663 UNDER FLOOR CONFIRMED IAW NDT MANUAL REV 124 PART 6 51-00-00 PROC 16 AND SERVICE BULLETIN 737-57A1296 REV 2. NO CRACKS FOUND IN REMAINING STRUCTURE. FABRICATED MADE REPAIR PART IAW DRAWING 65-45-410 REV H. INSTALLED IAW SRM REV 116 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

FOUND CRACKED INTERCOSTAL AT BS500A - 500B ABOVE S26L (FORWARD TOP CORNER OF INTERCOSTAL). CRACKED BAFFLE AT STA 500A-500B ABOVE STR 26L REPLACED WITH MADE REPAIR PART. PART FABRICATED IAW SRM REV 116 SECTION 51-50-01 MAT IDENTIFIED IAW 53-30-04 FIG 1 AND INSTALLED IAW 51-40-01.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

CORROSION AND BROKEN DOME NUT AFT CARGO PIT LOWER SKIN BETWEEN BS747 AND 767. CORRODED DOUBLER IN AFT CARGO PIT LOWER SKIN BETWEEN STA 747 AND 767 REPLACED. PART FABRICATED IAW SRM REV 116 SECTION 51-30-0 FIG 7 AND CORRODED DOME NUT AND DOUBLER INSTALLED IAW SAME SRM SECTION WITH RIVETS AND HI LOCKS IAW 51-40-02.

Part: BELTFRAME — GOUGED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

GOUGE/TOOLING DAMAGE ON THE BELT FRAME 887 RIGHT HAND AT UPPER FLANGE AT BS21R. GOUGE/TOOLING DAMAGE ON THE BELT FRAME 887 & 907 RT AT UPPER FLANGE AT STR 21R BOTH FRAMES REPLACED WITH NEW FRAMES IAW REPAIR INSTRUCTIONS DOC NR CS 23260-O/O DATED 9 MAY 2018.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,902 hrs · 51,637 cycles

CORROSION FOUND ON FRAME STA 1156 CORRODED AT LB 7 AND APPROX WL 224. CORRODED FRAME AT STA 1156 LBL 7 AND APPROX WL 224 REPAIRED IAW STA 1156 BULKHEAD FRAME CHORD REPAIR DWG R23260 1-053-015-001 REV NC.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

GOUGE ON FLOORBEAM WEB AT BS 344 LBL 2 ON AFT SIDE OF FRAME IN E&E BAY). REPAIR FLOORBEAM WEB AT STA 344 LBL 2 ON AFT SIDE OF FRAME IAW CS-23260-014 REV DATE: "-" / 23 MAY 2018.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 75,902 hrs · 51,637 cycles

CRACKED PRESSURE WEB ON INSIDE OF CABIN FOUND JUST AFT OF BS663, RBL 39, WL 202.6. CRACKED PRESSURE WEB ON INSIDE OF CABIN JUST AFT OF STA 663, RBL 39, WL 202.6 REPAIRED IAW SRM REV 116 SECTION 53-60-51 FIG 201.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

CRACKED STRINGER CLIP IN AFT PIT AT STA 727, STR 23L. REMOVED CRACKED STRINGER CLIP IN AFT CARGO PIT AT STA 727, STR 23L AND INSTALLED NEW STR CLIP P/N 65-51525-2 IAW SRM 51-40-02 PARA 4 REV 116.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

CRACK ON FUS SKIN BETWEEN BS727E AND 747 JUST BELOW S-24L. REPAIRED CRACK ON FUS SKIN BETWEEN STA 727E AND 747 JUST BELOW S-24L IAW SB737-53-1168 REV 4, PART 4 B.(3) AND SRM 53-00-01 REV 116 FIG 201 REPAIR 31 DETAIL VII.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 75,902 hrs · 51,637 cycles

BROKEN TAB ON STRINGER LIP REMOVED AT STA 500D LT SIDE STR 19. BROKEN TAB ON STRINGER CLIP AT STA 500D AND STR 19L REPLACED WITH MADE REPAIR PART. STRINGER CLIP FABRICATED IAW SRM REV 116 SECTION 51-30-01 PARA 8 AND INSTALLED WITH FASTENERS IAW 5-40-02 MAT IDENTIFIED IAW 53- 00-07 FIG 202.

Part: FLAP TRACK — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 74,173 hrs · 48,096 cycles

CORROSION NOTED AT LEFT INBOARD FLAP, INBOARD TRACK NR 4, FORWARD MOUNT POINT (BOTH SIDES). NR 4 TRACK REPLACED IAW AMM 27-51-27, REV. 83, PAGE 410.

Part: WINDOW FRAME — CRACKED (BS 520) · airframe 74,173 hrs · 48,096 cycles

CRACK FOUND AT BS 520, STRINGER 12R, UPPER FORWARD WINDOW CORNER. HFEC INSPECTION REVEALED 2 CRACKS IN THE WINDOW FRAME. WINDOW FRAME REPLACED IAW SERVICE BULLETIN 737-53A1177, REV. 7.

Part: WINDOW FRAME — CRACKED (BS 500A) · airframe 74,173 hrs · 48,096 cycles

CRACK FOUND AT BS 500A, STRINGER 12R, UPPER FORWARD WINDOW CORNER. HFEC INSPECTION REVEALED A CRACK IN THE WINDOW FRAME. WINDOW FRAME REPLACED IAW SERVICE BULLETIN 737-53A1177, REV. 7.

Part: WINDOW FRAME — CRACKED (BS 500B) · airframe 74,173 hrs · 48,096 cycles

CRACK FOUND AT BS 500B, S12R, UPPER FORWARD WINDOW CORNER. HFEC INSPECTION REVEALED A CRACK IN THE WINDOW FRAME. WINDOW FRAME REPLACED IAW SERVICE BULLETIN 737-53A1177, REV. 7.

Part: WINDOW FRAME — CRACKED (BS 787) · airframe 74,173 hrs · 48,096 cycles

CRACK FOUND AT BS 787, STRINGER 13L, LOWER FORWARD WINDOW CORNER. HFEC INSPECTION REVEALED A CRACK IN THE FUSELAGE SKIN AND THE WINDOW FRAME. CRACKED SKIN REPAIRED IAW SRM 53-00-01 REV. 111, REPAIR 34. THE WINDOW FRAME REPLACED IAW SERVICE BULLETIN 737-53A1177, REV. 7.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 74,173 hrs · 48,096 cycles

CRACK NOTED ON AFT PRESSURE BULKHEAD, BS1016, GORE WEB NR 6. CRACK REPAIRED IAW SRM, REV 111, 53-80-08, REPAIR 9.

Part: BULKHEAD WEB — CRACKED (BS 1016) · airframe 74,173 hrs · 48,096 cycles

CRACK NOTED ON AFT PRESSURE BULKHEAD, BS 1016. REPAIRED IAW SRM 53-80-08, REV 111, REPAIR 9.

Part: SKIN — CRACKED (BS 827) · airframe 74,173 hrs · 48,096 cycles

CRACK FOUND AT BS 827, STRINGER 12L, UPPER AFT WINDOW CORNER. HFEC INSPECTION REVEALED 2 CRACKS IN THE FUSELAGE SKIN. CRACKS IN SKIN REPAIRED IAW SERVICE BULLETIN 737-53A1177, REV. 7.

Part: SKIN — CRACKED (WINDOW BELT) · airframe 74,173 hrs · 48,096 cycles

CRACK FOUND AT BS 867, STRINGER 13L, LOWER FORWARD WINDOW CORNER. HFEC INSPECTION REVEALED A CRACK IN THE FUSELAGE SKIN. CRACKED SKIN REPAIRED IAW SRM 53-00-01, REV. 111, REPAIR 34 AND SERVICE BULLETIN 737-53A1177, REV.7.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 74,173 hrs · 48,096 cycles

CRACK NOTED ON AFT PRESSURE BULKHEAD, BS1016, FORWARD SIDE BETWEEN S6L AND S7L. CRACK REPAIRED IAW SRM, REV 111, 53-80-08, FIGURE 201, REPAIR 7.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,173 hrs · 48,096 cycles

CRACK NOTED ON STRINGER S4L AT BS559. CRACK REPAIRED IAW SRM, REV 111, 53-00-03, FIGURE 201, REPAIR 4.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 74,173 hrs · 48,096 cycles

STIFFENER FOUND CRACKED AT BS291, S10R. REPLACED STIFFENER WITH MADE PART IAW DRAWING 65-45807, REV AG. INSTALLED PART IAW SRM, REV 111, 51-40-02.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 74,173 hrs · 48,096 cycles

CRACK NOTED ON AFT PRESSURE BULKHEAD, BS1016, GORE WEB NR7. CRACK REPAIRED IAW SRM, REV 111, 53-80-08, REPAIR 9.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 74,173 hrs · 48,096 cycles

STRINGER SPLICE CRACK NOTED AT BS908, S14L. REPLACED STRINGER SPLICE WITH MADE PART IAW DRAWING 65-45778, REV L. INSTALLED PART IAW SRM REV 111, 51-40-02.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 74,173 hrs · 48,096 cycles

STRINGER SPLICE CRACK NOTED AT BS908, S10R. REPLACED STRINGER SPLICE WITH NEW PART IAW SRM REV 111, 51-40-02.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 74,173 hrs · 48,096 cycles

RIGHT HAND INBOARD TRAILING EDGE AFT FLAP DELAMINATED ALONG AFT EDGE ON LOWER SURFACE. REPAIRED IAW SRM, REV 111, 51-70-10, REPAIR 4, PAGE 214, FIGURE 202, ITEM H.

Part: LINK ASSY — CORRODED (LT MLG) · corrosion level 2 · airframe 74,173 hrs · 48,096 cycles

LEFT HAND MAIN LANDING GEAR SUPPORT BEAM, INBOARD END, FUSELAGE ATTACHMENT LINK ASSEMBLY HAS EVIDENCE OF CORROSION. CORROSION FOUND TO BE BEYOND ALLOWABLE CMM LIMITS. LINK ASSEMBLY REPLACED WITH OVERHAULED, SERVICEABLE PART IAW AMM 57-15-00, REV 83.

Part: LINK ASSY — CORRODED (RT MLG) · corrosion level 2 · airframe 74,173 hrs · 48,096 cycles

RIGHT HAND MAIN LANDING GEAR SUPPORT BEAM, INBOARD END, FUSELAGE ATTACHMENT LINK ASSEMBLY HAS EVIDENCE OF CORROSION. CORROSION FOUND TO BE BEYOND ALLOWABLE CMM LIMITS. LINK ASSEMBLY REPLACED WITH NEW PART IAW AMM 57-15-00, REV 83.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,173 hrs · 48,096 cycles

EXISTING REPAIR REMOVED FOR INSPECTION AT BS332.10, R1 DOOR LOWER AFT CORNER. INSPECTED FUSELAGE SKIN AND REPAIRED UNDERLYING DAMAGE IAW SRM REV 111, 53-10-01, FIGURE 201, REPAIR 2.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,173 hrs · 48,096 cycles

FORWARD WASTE SERVICE PANEL MESH HEATER AND DOUBLER BEHIND VALVE ARE CORRODED. FORWARD WASTE SERVICE PANEL MESH HEATER GASKET BEHIND VALVE REPLACED IAW AMM 38-32-81, REVISION 83. DOUBLER BEHIND VALVE REPLACED IAW SRM 51-40-02, REVISION 111.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,173 hrs · 48,096 cycles

CRACK FOUND IN HOLE AT BS887, S13L, LOWER FORWARD WINDOW CORNER. HFEC INSPECTION REVEALED A CRACK IN THE FUSELAGE SKIN. CRACKED SKIN REPAIRED IAW SRM REV 111, 53-00-01, REPAIR 34 AND SERVICE BULLETIN 737-53A1177, REV 7.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,173 hrs · 48,096 cycles

CRACK FOUND ON FRAME AT BS493, S18R TO S25R FORWARD CARGO DOOR CUTOUT, AFT SURROUND FRAME. REPLACED FRAME WITH NEW PART IAW DRAWING 65-20723, REV AB. FASTENERS INSTALLED IAW SRM, REV 111, 51-40-02.

Part: SKIN — CRACKED (396) · airframe 74,173 hrs · 48,096 cycles

CRACK FOUND IN SKIN AT BS 396, STRINGER 13R, LOWER AFT WINDOW CORNER. THE SKIN WAS REPAIRED IAW ENGINEERING REPAIR INSTRUCTION, CS-23260-004.

Part: SKIN — CRACKED (BS 376) · airframe 74,173 hrs · 48,096 cycles

CRACK FOUND IN SKIN AT BS 376, S13R, LOWER AFT WINDOW CORNER DURING AN HFEC INSPECTION. THE SKIN WAS REPAIRED IAW ENGINEERING REPAIR INSTRUCTIONS, CS-23260-004.

Part: SUPPORT FITTING — CRACKED (LT MLG) · airframe 74,173 hrs · 48,096 cycles

DURING ACCOMPLISHMENT OF OPEN HOLE INSPECTION IAW AD 2014-12-13, FOUND CRACK IN HOLE NR 5 OF THE AFT SUPPORT FITTING FOR THE LEFT HAND MAIN LANDING GEAR SUPPORT BEAM. REPLACED SUPPORT FITTING WITH A NEW PART IAW SERVICE BULLETIN 737-57A1318, REV 1 AND SRM REV 111, 51-40-02.

Part: SUPPORT FITTING — CRACKED (RT MLG) · airframe 74,173 hrs · 48,096 cycles

DURING ACCOMPLISHMENT OF OPEN HOLE INSPECTION IAW AD 2014-12-13. FOUND CRACKS IN HOLE NR 5 OF THE AFT SUPPORT FITTING FOR THE RIGHT HAND MAIN LANDING GEAR SUPPORT BEAM. REPLACED SUPPORT FITTING WITH A NEW PART IAW SERVICE BULLETIN 737-57A1318, REV 1 AND SRM REV 111, 51-40-02.

Part: ATTACH BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 74,173 hrs · 48,096 cycles

RIGHT HAND INBOARD TRAILING EDGE FORE FLAP, CENTER ATTACH BRACKET, AFT BORE AND FACES FOUND TO BE CORRODED BEYOND LIMITS. REMOVED AND REPLACED CENTER ATTACH BRACKET IAW CMM 57-53-24, REVISION 51.

Part: SKIN — GOUGED (BS 854) · airframe 74,173 hrs · 48,096 cycles

GOUGES ON LOWER FUSELAGE SKIN BELOW AFT CARGO DOOR, BS 854, S24R TO S25R. REPAIRED IAW SR 4-3473379396.

Part: SKIN — CRACKED (FUSELAGE)

WHILE PERFORMING AD 2013-18-08, A 1" CRACK WAS FOUND AT BS 500D +18.5 BELOW S12L. THERE IS AN INTERNAL PREVENTIVE MODIFICATION AT THIS LOCATION. TEMP REPAIR INSTALLED IAW MESSAGE NAC-16-0014-10B.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,005 hrs · 47,741 cycles

WHILE PERFORMING AD 2013-18-08, S, 2, A 2" CRACK WAS DISCOVERED AT BS727E S22R.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,005 hrs · 47,741 cycles

WHILE PERFORMING AD 2013-18-08, A 2" CRACK WAS DISCOVERED AT BS727E S22R. REPAIRED CRACK IAW SRM 53-00-01, REPAIR 21, DETAIL X, CAT B INSPECTIONS ADDED TO INSPECTION PROGRAM.

Part: FAILSAFE — CRACKED (BS 480) · airframe 73,465 hrs · 57,254 cycles

FWD CARGO BAY HAS A CRACKED FAILSAFE BS 480 AND STR 25L.

Part: FAILSAFE — CRACKED (BS 460) · airframe 73,465 hrs · 57,254 cycles

FWD CARGO PIT HAS CRACKED FAIL SAFE AT BS 460, STR 25L.

Part: INTERCOSTAL — CRACKED (BS 500D-520) · airframe 72,381 hrs · 46,135 cycles

AIR CONDITIONING SNAKE PIT BS500D TO BS520 AT CENTER LINE OF FUSELAGE, INTERCOSTAL CRACKED AT AFT FLANGE RADIUS. REPLACED INTERCOSTAL WITH FABRICATED WEBB REF: IAI SUPP 53-30-51, DETAIL 1, FIG 1. INSTALLED IAW SRM 51-40-3.

Part: CHANNEL — CORRODED (BS 797-847) · corrosion level 2 · airframe 72,074 hrs · 45,961 cycles

CORROSION UNDER THRESHOLD PLATE, AFT CARGO DOORWAY AT BS807 ON THRESHOLD CLOSURE CHANNEL. REPLACED THRESHOLD CLOSURE CHANNEL, PN 65-47957-10 AT AFT CARGO DOORWAY BS797-BS847 IAW DWG 65-47957, REV D.

Part: BULKHEAD — CRACKED (NLG WW) · airframe 72,074 hrs · 45,961 cycles

UPPER WEB OF NLG WHEEL WELL CRACKED AT RT ACCESS PANEL CUTOUT AFT INBD CORNER BS251, RBL3. CRACKED UPPER WEB OF NLG PN 65-45819-121, R & R WITH NEW PART IAW SRM 51-40-02, REV 104.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 72,074 hrs · 45,961 cycles

RIGHT HORIZONTAL STABILIZER OTBD RIB AT BS295.10 HAS CRACKED LOWER CHORD, FWD END INBD FLANGE. REPLACED LOWER CHORD WITH A MADE PART IAW SRM REV 104, CH 51-10-02, PARA 8 AND 51-30-01.

Part: SKIN — CORRODED (BS 986-1006) · airframe 72,074 hrs · 45,961 cycles

CORROSION ON OUTER SURFACE OF FUSELAGE SKIN AT AFT DRAIN MAST, BS 986.5-1006, S24-25L. REPAIRED IAW FAA FORM 8100-9, REF ID 201409170163-0002D1 & SERVICE REQUEST 4-2696701871.

Part: RIB — GOUGED (HORIZONTAL STAB) · airframe 72,074 hrs · 45,961 cycles

RIGHT HORIZONTAL STAB OTBD CLOSURE RIB T/E SECTION CORRODED AND GOUGED. RIGHT HORIZONTAL STAB OTBD CLOSURE RIB T/E SECTION REPLACED WITH A MADE REPAIR PART FABRICATED IAW SRM REV 104, CH 51-30-01, MATERIAL IDENTIFICATION IAW SRM REV 104, CH 55-10-09, FIG 1 AND FASTENER INSTALL IAW SRM REV 104 51-40-02.

Part: INTERCOSTAL — CRACKED (BS 440-460) · airframe 72,074 hrs · 45,961 cycles

CRACKED INTERCOSTAL AT BS440 - BS460, BL6R IN FORWARD CARGO PIT. REPLACED CRACKED INTERCOSTAL AT STA440-460, RBL6 IN FWD CARGO PIT WITH A MADE REPAIR PART IAW SRM 51-10-07, 51-30-01, AND 51-40-02, REV 104. REF MCO: 0001002513 AND WO 1324876.

Part: INTERCOSTAL — DAMAGED (BS 460-500) · airframe 72,074 hrs · 45,961 cycles

HOLES ENLARGED IN INTERCOSTAL AT BS460-BS480 AND BS480-BS500, S28R. INTERCOSTAL AT STA 460-480 AND 480-500, STR 28R REPLACED WITH MADE REPAIR PARTS FABRICATED IAW SRM, REV 104 51-30-01, MATERIAL IDENTIFICATION DONE IAW SRM REV 104, 53-30-15, DETAIL I. FASTENERS INSTALLED IAW SRM REV 104, 51-40-02 REF: 0001002513, WO 1326714 AND 1317146.

Part: PLATE — CORRODED (BS 934-951) · corrosion level 2 · airframe 72,074 hrs · 45,961 cycles

CORROSION ON SILL PLATE BS934-BS951, RBL56. REMOVED CORROSION ON SILL PLATE AT BS934-BS951, RBL56. CORROSION BEYOND LIMITS IAW SRM REV 104, CH 51-10-02, PARA 14. REPLACED SILL PLATE IAW SRM, REV 104, CH 51-40-02 & CH 51-10-02, PARA 10.

Part: KEELBEAM — CORRODED (BS 685-727) · corrosion level 2 · airframe 72,074 hrs · 45,961 cycles

INSPECTION NOTED FRETTING CORROSION AND PITTING CORROSION UNDER NUT PLATES ON THE PANEL MOUNTING TANG OF THE KEELBEAM, LOWER OTBD CHORD. BLENDED OUT OF LIMITS. REPAIRED IAW TASS DOCUMENT 121058-R021, REV 5, REF MCO 0001002513, WO 1320443.

Part: FLOORBEAM — CORRODED (BS 927) · corrosion level 2 · airframe 72,074 hrs · 45,961 cycles

CORROSION ON FLOORBEAM BS 927, RBL46-60. CORROSION BEYOND LIMITS IAW SRM, REV 104, 51-10-02, PG 12, PARA 14. REPAIRED, BLENDED OUT CORROSION ON FLOORBEAM, IAW SRM REV 104 53-60-51, FIG 201, REPAIR 2.

Part: SKIN — DAMAGED (BS 294-312) · airframe 72,074 hrs · 45,961 cycles

FUSELAGE SKIN DAMAGED AT BS 294-BS 312, STR 21R. REPAIRED FUSELAGE SKIN AT BS 294-BS 312, STR 21R IAW SRM 53-00-01, REPAIR 31, DETAIL VIII, REV 104.

Part: TEE FITTING — CRACKED (HORIZONTAL STAB) · airframe 72,074 hrs · 45,961 cycles

RIGHT HORIZONTAL STABILIZER, HSS285.90 AT LT AFT OF FWD SPAR, CRACKED ON "T"-SECTION. CRACKED "T"-SECTION, LOWER CHORD, ON RT HORIZONTAL STAB RIB AT HSS285.90 REPAIRED IAW SRM REV 104, 55-10-09, FIG 201, REPAIR 2.

Part: FLOORBEAM — CORRODED (BS 328) · corrosion level 2 · airframe 72,074 hrs · 45,961 cycles

CORROSION ON TOP CAP OF FLOORBEAM AT STA328, RBL45 WAS FOUND BEYOND LIMITS IAW REV 104, SRM CHAPTER 51-10-02, PARA 14. REPLACED TOP CAP IAW SRM REV 104, CHAPTER 53-10-51, REPAIR 5 AND CHAPTER 51-40-02, REF MCO: 0001002513, WO 1321026.

Part: TEE FITTING — CRACKED (HORIZONTAL STAB) · airframe 72,074 hrs · 45,961 cycles

RIGHT HORIZONTAL STABILIZER, HSS92.70 AT L/E AFT SIDE OF FWD SPAR CRACKED ON "T"-SECTION. REPAIRED RIGHT HORIZONTAL STAB HSS92.70 AT L/E AFT SIDE OF FWD SPAR IAW SRM, REV 104, CH 55-10-09, REPAIR 2.

Part: STRAP — CORRODED (BS 780) · corrosion level 2 · airframe 72,074 hrs · 45,961 cycles

STRAP CORRODED AT LWR FWD CORNER OF AFT CARGO DOOR FRAME BS780, RBL20. REPLACED BY NEW PN 69-43456-2, STRAP FILLER IAW SRM 51-40-02, REV 104.

Part: STIFFENER — CRACKED (BS 1016) · airframe 72,074 hrs · 45,961 cycles

CRACKED HOLE ON "Z" STIFFENER FLANGE AT DOME CAP IN THE CENTER OF THE AFT PRESSURE BULKHEAD. REPAIRED "Z" STIFFENER FLANGE AT DOME CAP IN THE CENTER OF THE AFT PRESSURE BULKHEAD IAW SERVICE REQUEST 4-2708852928. REF: FAA FORM 8100-9, ID 201409220057-0004D1.

Part: FRAME — CRACKED (ZONE 100) · airframe 70,049 hrs · 44,508 cycles

E/E BAY, A CRACKED FRAME WEB AT BS 328 BETWEEN STRINGER 20-21R. REMOVED CRACKED FRAME IAW SRM 51-40-02. INSTALLED NEW FRAME IAW SRM.

Part: SUPPORT BRACKET — CRACKED (ZONE 200) · airframe 70,049 hrs · 44,508 cycles

CRACK IN RADIUS OF SUPPORT BRACKET FOR COCKPIT VOICE RECORDER. REMOVED CRACKED SUPPORT BRACKET AND FABRICATED NEW SUPPORT BRACKET IAW SRM 51-30-01. INSTALLED SUPPORT BRACKET IAW SRM 51-40-05.

Part: SKIN — SCRATCHED (ZONE 200) · airframe 70,049 hrs · 44,508 cycles

SCRATCH FOUND IN "EXTRA SENSITIVE AREA" OF THE RIGHT STATIC PORT. BURNISHED AREA TO REMOVE SCRATCH IAW SRM 53-00-01. PERFORMED AN NDT INSPECTION TO DETERMINE MATERIAL LOST, IAW ASTM E 797, AREA FOUND TO BE WITH IN LIMITS.

Part: SKIN — CRACKED (ZONE 100) · airframe 700,049 hrs · 44,508 cycles

EXTERIOR FUSELAGE SKIN IS CRACKED AT CUTOUT OF GROUND AIR CONDITIONING RECEPTACLE AT BS 520. ROUTED OUT SKIN TO REMOVE CRACK IAW SRM 51-10-02. NDT INSPECTION WAS CONDUCTED TO VERIFY NO ADDITIONAL CRACKING OF SKIN WAS PRESENT IAW NDT MANUAL 51-00-00, NO CRACKS NOTED. REPAIR WAS ACCOMPLISHED IAW DRAWING 53-12221-1, NEW REV.

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 70,049 hrs · 44,508 cycles

CORROSION ON LAVATORY WALL SUPPORT IN FORWARD CABIN. REMOVED CORRODED FORWARD LAVATORY WALL SUPPORT IAW SRM 51-40-2. FABRICATED AND INSTALLED FORWARD LAVATORY WALL SUPPORT IAW SRM 51-40-02.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 70,049 hrs · 44,508 cycles

ELECTRONIC COMPARTMENT, CORROSION ON SECTION OF STRINGER 24L BS 344 - 360. REMOVED CORRODED STRINGER. FABRICATED FILLERS AND REPAIR ANGLES IAW SRM 51 -00-03. INSTALLED REPAIR IAW SRM 51-40-02.

Part: BAFFLE — CRACKED (BS 500B-500C) · airframe 70,049 hrs · 44,508 cycles

CRACK IN THREE LIGHTING HOLES AT BS 500B TO 500C STRINGER 26 RIGHT IN FORWARD BAGGAGE COMPARTMENT. REMOVED CRACKED BAFFLE IN FORWARD BAGGAGE COMPARTMENT IAW SRM 51-40-02. FABRICATED NEW BAFFLE IAW SRM 51-30-01. INSTALLED BAFFLE IN FORWARD BAGGAGE COMPARTMENT IAW SRM 51-40-02.

Part: STRUCTURE — CORRODED (ZONE 100) · corrosion level 2 · airframe 70,049 hrs · 44,508 cycles

ELECTRONIC COMPARTMENT, STRINGER END AT TERMINATION HAS CORROSION AT BS 360 AND STRINGER 25R. REMOVED CORRODED PARTS IAW SRM 53-00-03. REMOVED FASTENERS COMMON TO STRING 25R, AND VERIFIED NO ADDITIONAL CORROSION. FABRICATED ALL REPAIR PARTS IAW SRM 53-00-03. INSTALLED ALL REPAIR CHANNELS IAW SRM 53-00-03.

Part: SKIN — CANNING (ZONE 100) · airframe 70,049 hrs · 44,508 cycles

EXTERIOR FUSELAGE BELLY "OIL CANNING" SKIN BETWEEN BODY STATION 1016 AND 1044, APPROXIMATELY STRINGER 27L AND 27R. VERIFIED "OIL CANNING" WAS OUT OF LIMITS. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-80-01 AND 53-88-01.

Part: DRAIN — CORRODED (ZONE 900) · corrosion level 2 · airframe 70,049 hrs · 44,508 cycles

CORROSION ON FLOOR DRAIN LINE FITTING AND SURROUNDING STRUCTURE AT BS 1086.5, REMOVED CORRODED PLATE AND DRAIN LINE FITTING. FABRICATED NEW FILLER PLATES IAW SRM 51-40-05. INSTALLED FILLER PLATES IAW SRM 51-40-02. INSTALLED NEW DRAIN FITTING IAW SRM 51-40-02.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 70,049 hrs · 44,508 cycles

ELECTRONIC COMPARTMENT, CORROSION ON SHEAR TIE BS 344 STRINGER 27R. REMOVED CORRODED SHEAR TIE IAW SRM 51-40-02. FABRICATED SHEAR TIE AND FRAME FLANGE AND ALL REPAIR PARTS IAW SRM 53-00-07 AND 51-30-01. INSTALLED IAW SRM 53-00-07.